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 -LAST LEG REPORT The purpose of this item is to present the fault messages (class 1 and 2, internal and external) that appeared during the last flight.
 -PREVIOUS LEGS REPORT The purpose of this item is to present the fault messages (class 1 and 2, internal and external) that appeared during the previous flights. When no fault has been detected during the last 63 flights, the NO FAULT DETECTED message is displayed.
 -LRU IDENTIFICATION The purpose of this item is to present the Part Number (PN), the Serial Number (SN) and the Software Number (SW/N) of the component.
 -TROUBLE SHOOTING DATA This item allows to analyze the snapshot of the recorded failure to detect the software bugs.
 -CLASS 3 FAULTS The purpose of this item is to present the class 3 fault messages that appeared during the last flight. There is no date and no failure classification.
 -GROUND REPORT The purpose of this item is to present the class 1, 2 or 3 internal failures when they are detected on ground.
 -DISCRETE CONFIGURATION The purpose of this item is to present many information of program pins dedicated to the ATC system installation.
 -TEST The activation of this manual test shall only be allowed on the ground. The results of the test are transmitted to the CFDIU but are not memorized.
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 ATC Maintenance Test Procedure - ATC Menu (sheet 9/9)
 Figure 017A

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 ATC Maintenance Test Procedure - ATC Menu (sheet 6/9)
 Figure 018

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 ATC Maintenance Test Procedure - ATC Menu (sheet 7/9)
 Figure 019

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 ATC Maintenance Test Procedure - ATC Menu (sheet 8/9)
 Figure 020

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 --------------------------------------------------------------------------| REPORTED INTERNAL FAILURES | |------------------------------------------------------------------------| | MESSAGE (i = 1 or 2) | CLASS | ATA | |---------------------------------------------|---------|----------------| | ATCi (1SHi) | 1 | 34-52-33 | | ATC1 TOP ANTENNA (7SH3) | 1 | 34-52-11 | | ATC1 BOT ANTENNA (7SH1) | 1 | 34-52-11 | | ATC2 TOP ANTENNA (7SH4) | 1 | 34-52-11 | | ATC2 BOT ANTENNA (7SH2) | 1 | 34-52-11 | | WRG : MODE S ADRESS/ATCi (1SHi) | 1 | 34-52-33 | --------------------------------------------------------------------------
--------------------------------------------------------------------------| REPORTED EXTERNAL FAILURES | |------------------------------------------------------------------------| | MESSAGE (i = 1 or 2) | CLASS | ATA | |---------------------------------------------|---------|----------------| | ATC CTL PNL (3SH)/ATCi (1SHi) | 1 | 34-52-12 | | ADIRU i/3(1FPi/3)/ATCi (1SHi) | 1 | 34-12-34 | | TCAS(1SG)/ATCi(1SHi) | 3 | 34-43-34 | | CFDIU(1TW)/ATCi(1SHi) | 3 | 31-32-34 | | FMGCi(1CAi)/ATCi(1SHi) | 3 | 22-83-34 | | POWER SUPPLY INTERRUPT | 1 | 24-00-00 | | LGCIUi(5GAi)/ATCi(1SHi) | 3 | 32-31-71 | --------------------------------------------------------------------------
R 1EFF : 106-149, 221-299, 301-399, 401-499, 1 34-52-00Page 99 1 1 Aug 01/05 1 1 1CES 1 1EFF : 201-220, 1 34-52-00Page A0 1 1 May 01/05 1 1 1CES 1 1EFF : 201-220, 1 34-52-00Page A1 1 1 May 01/05 1 1 1CES 11EFF : 201-220, 1 34-52-00Page A2 1 1 May 01/05 1 1 1CES 11EFF : 051-099, 1 34-52-00Page A3 1 1 May 01/05 1 1 1CES 1 When the selected system on the ATC control unit is different from the system under test, this causes illumination of a message on the MCDU after the TEST selection. This message is: PLEASE CHECK IF THE CONTROL PANEL SWITCH IS ON SYSTEM (1 OR 2) AND PRESS TEST KEY. Reminder: The TEST pushbutton switch is used to initiate the LED test and transponder self-test. When this pushbutton switch is pressed while the LEDs are still on, the next previous flight leg is displayed. The transponder has the capability to store 10 flight legs. To display all stored flight legs, the pushbutton switch must be pushed when the previous flight leg is being displayed. When all flight legs are displayed, all LEDS flash to indicate the end of the routine.

R  **ON A/C 201-220, 
R  A. CFDIU Interface 
R  (1) BITE description 
R  The BITE facilitates maintenance on in-service aircraft. It detects 
R  and identifies a failure related to the ATC system. 
R  The BITE of the ATC transponder is connected to the CFDIU. 
R  The unit tested is the ATC transponder. 
　
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